View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 39439U 13066Z 24337.70503064 .00040832 00000-0 23592-2 0 9998
2 39439 97.7304 301.2253 0031525 287.1581 72.6198 15.11748675596226
| Epoch (UTC): | 02 December 2024 16:55:14 |
| Eccentricity: | 0.0031525 |
| inclination: | 97.7304° |
| perigee height: | 509 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 301.2253° |
| argument of perigee: | 287.1581° |
| revolutions per day: | 15.11748675 |
| mean anomaly at epoch: | 72.6198° |
| orbit number at epoch: | 59622 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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